Accession Number : ADB057257
Title : Evaluation of High Temperature Damping Applications to Increase Fatigue Life in Rotating Jet Engine Components.
Descriptive Note : Final rept. May 79-Aug 80,
Corporate Author : DAYTON UNIV OH RESEARCH INST
Personal Author(s) : Drake,Michael L. ; Dominic,Robert J. ; Kumar,Binod
Report Date : DEC 1980
Pagination or Media Count : 324
Abstract : The purpose of this particular program was to: establish the feasibility of using enamels to control HCF by controlling resonant vibration in rotating turbomachinery; establish probable damping design approaches for the generic structure involved; and determine research areas covering all phases of the program which will need substantial efforts to advance the enamel damping state-of-art to a point where the enamel damping approach to HCF control is a practical alternative in rotating turbomachinery design.
Descriptors : *Fatigue(Mechanics), *Damping, *Enamels, *Rotor blades(Turbomachinery), Turbofan engines, Thermal fatigue, Disks, Ceramic coatings, Vibration, Resonance, Engine components, High rate, Rotation, Fatigue life, High temperature, Thermal stresses
Subject Categories : Ceramics, Refractories and Glass
Jet and Gas Turbine Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE